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gptkbp:instanceOf
|
turbofan engine
|
|
gptkbp:aircraft
|
Hawk_family
|
|
gptkbp:application
|
trainer aircraft
|
|
gptkbp:controls
|
FADEC
|
|
gptkbp:coolingSystem
|
air-cooled
|
|
gptkbp:countryOfOrigin
|
gptkb:United_Kingdom
|
|
gptkbp:design
|
modular design
|
|
gptkbp:designedBy
|
gptkb:Rolls-Royce
|
|
gptkbp:diameter
|
0.9 m
|
|
gptkbp:emissionsStandard
|
ICAO_Chapter_4
|
|
gptkbp:engine
|
1.5 m
300 kg
pylon-mounted
air starter
|
|
gptkbp:engineConfiguration
|
twin-spool
|
|
gptkbp:engineDisplacement
|
0.9 m
|
|
gptkbp:enginePower
|
3,500 lbf
|
|
gptkbp:engineType
|
turbofan engine
afterburning turbofan
axial compressor
single-stage turbine
|
|
gptkbp:firstFlight
|
1970s
|
|
gptkbp:fuelCapacity
|
0.8 kg/s
|
|
gptkbp:fuelType
|
gptkb:Jet_A-1
annular combustor
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Adour Mk 171-26
|
|
gptkbp:length
|
1.5 m
|
|
gptkbp:maintenance
|
1,000 hours
|
|
gptkbp:maxSpeed
|
Mach_0.9
|
|
gptkbp:noise_level
|
85 dB
|
|
gptkbp:notableUsers
|
gptkb:Indian_Air_Force
gptkb:Royal_Air_Force
gptkb:Royal_Australian_Air_Force
gptkb:South_African_Air_Force
gptkb:Saudi_Arabian_Air_Force
|
|
gptkbp:numberOfStudents
|
5
|
|
gptkbp:operationalArea
|
military training
|
|
gptkbp:operationalStatus
|
in service
|
|
gptkbp:propulsion
|
11.67:1
approximately 3,500 lbf
|
|
gptkbp:related_engine
|
Brayton_cycle
|
|
gptkbp:services
|
1980s
|
|
gptkbp:successor
|
gptkb:Adour_Mk_151
|
|
gptkbp:type
|
military aircraft engine
|
|
gptkbp:usedIn
|
gptkb:BAE_Systems_Hawk
|
|
gptkbp:weight
|
approximately 300 kg
|